Kh-20 / AS-3 KANGAROO
| Specifications | ||
|---|---|---|
| Contractor | ||
| Type | meduim- to long-range standoff missile | |
| Initial operational capability | 1960 | |
| First detected by West | 1961 | |
| Production terminated | 1965 | |
| Wingspan | 9.2 m | |
| Length | 14.9 m | |
| Diameter | 1.9 m | |
| Launch weight | 11000 kg | |
| Max. speed | 2280 km/h | |
| Ceiling | 18000 m | |
| Maximum range | 650 km | |
| Propulsion | Tumansky R-11 twin spool turbojet with afterburner | |
| Thrust | 50.9 kN of thrust | |
| Guidance | beam riding | |
| Warhead | ||
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